EP0540594A1 - Verfahren und vorrichtung zur richtungsmessung - Google Patents

Verfahren und vorrichtung zur richtungsmessung

Info

Publication number
EP0540594A1
EP0540594A1 EP91913367A EP91913367A EP0540594A1 EP 0540594 A1 EP0540594 A1 EP 0540594A1 EP 91913367 A EP91913367 A EP 91913367A EP 91913367 A EP91913367 A EP 91913367A EP 0540594 A1 EP0540594 A1 EP 0540594A1
Authority
EP
European Patent Office
Prior art keywords
image
source
detector
forming
transit
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP91913367A
Other languages
English (en)
French (fr)
Inventor
Technology Group Limited British
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BTG International Ltd
Original Assignee
BTG International Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BTG International Ltd filed Critical BTG International Ltd
Publication of EP0540594A1 publication Critical patent/EP0540594A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S3/00Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/78Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
    • G01S3/782Systems for determining direction or deviation from predetermined direction
    • G01S3/787Systems for determining direction or deviation from predetermined direction using rotating reticles producing a direction-dependent modulation characteristic

Definitions

  • This invention relates to a method and apparatus for measurement of the direction, from a position at which the measurement is made, of an observed object or target, such measurement being thus comparable with directional measurements made by use of a theodolite.
  • a conventional theodolite comprises a telescope, mounted to be rotatable about vertical and horizontal axes, and horizontal and vertical circular scales against which the angular position of the telescope can be measured, after It has been aligned on a remote target, to give a first reading related to the bearing or azimuthal direction of the target from the theodolite location and a second reading representing the elevatlonal angle of the target above or below the horizontal.
  • Such a theodolite requires the co-operation of a human observer, both for aligning the telescope on the target and for reading the azimuthal and elevatlonal data from the circular scales.
  • a "suitable" target for the purposes of the Invention, 1s one which is, effectively, a point source of electromagnetic radiation, preferably but not necessarily 1n the visible or 1R part of the spectrum. In practice, at a range in excess of about 3 metres even an ordinary torch bulb qualifies as a suitable target.
  • a direction-measuring instrument for measuring the direction of a remote source of radiation
  • the instrument comprising support means, a detector head rotatably mounted thereon for rotation about a fixed axis, and position-indicating means which provides an output signal Indicating the rotational position of the detector head
  • the detector head being provided with detector means sensitive to radiation emitted by the remote source and with means for forming an image of the source which transits across the detector means as the detector head rotates
  • the image-forming means being such that the image comprises two line-image components which extend transversely to the transit direction and which are oppositely inclined to that direction
  • the detector means being arranged, in response to the transit across 1t of each line-image component, to cause the instantaneous angular position of the detector head as indicated by the position indicating means to be recorded
  • computing means which derives two component measurements of the direction of the source from, respectively, the mean of the two recorded angular positions and the difference between them.
  • the means for forming an image comprises a pair of elongate cylindrical lenses mounted with their long axes oppositely skewed relative to the axis of rotation of the detector head and forming, of a distant source, correspondingly oppositely skewed line Images which transit across the detector means as the detector head rotates.
  • the means for forming an image comprises a pair of elongate concave cylindrical mirrors mounted with their long axes oppositely skewed relative to the axis of rotation of the detector head and forming, of a distant source, correspondingly oppositely skewed line images which transit across the detector means as the detector head rotates.
  • a method of measuring the direction of a remote source of radiation comprising providing, in fixed relationship to one another and rotatable together about a fixed axis, detector means sensitive to radiation emitted by the source and image-forming means, forming by means of the image-forming means an image of the remote source, said image comprising two line-image components oppositely skewed with respect to said fixed axis, rotating the detector means and the image-forming means together about the said fixed axis and thereby causing the two I1ne-1mage components of the image to transit across the detector means, recording the two angular positions of the detector means and image-forming means at which the respective Une-image components transit across the detector means, and deriving two component measurements of the direction of the source from, respectively, the mean of the two recorded angular positions and the difference between them.
  • Figure 1 is a diagrammatic perspective view of a stationary base or support and a rotatable sensor head of a direction measuring instrument 1n accordance with the Invention;
  • Figure 2 is a diagrammatic horizontal sectional view of the sensor head shown 1n Figure 1, showing also a remote target In respect of which directional information is to be measured;
  • Figures 3(1), (11) and (111) are diagrams relating to measurement of the elevatlonal direction of the target;
  • Figure 4 illustrates a refinement In detector means of the instrument shown in Figures 1 and 2;
  • Figure 5 is a representation of an output signal produced by detector means in accordance with Figure 4 incorporated In an instrument otherwise in accordance with Figures 1 and 2;
  • Figure 6 is comparable with Figure 2 and Illustrates another embodiment of a sensor head of an instrument according to the invention.
  • the sensor head represented In Figure 1 and indicated generally by reference numeral 10 comprises a cylindrical housing
  • a tripod or other stationary support IT to be rotatable about an axis 1-1 of the housing, and the support is provided with adjustment means (not shown) for setting the axis 1-1 vertical.
  • a circular angle-encoder scale 12 Secured to the base of the housing 11 for rotation therewith 1s a circular angle-encoder scale 12 which co-operates with a stationary reader device (not shown), mounted on the stationary support IT, to provide an electrical output signal indicative of the angular position of the head 10 at any given time.
  • a pair of cylindrical lenses 13 and 14 Mounted in the cylindrical wall of the housing 11 are a pair of cylindrical lenses 13 and 14, of which the long axes are oppositely skewed relative to the axis 1-1 so that the two lenses are in a symmetrical 1nverted-V configuration.
  • a photosensor 15 1s mounted with its sensitive surface directed towards a point midway between the midpoints of the two lenses, so that it is exposed to both lenses equally.
  • the lenses are of such focal length that each will produce, from a remote point object aligned with the photosensor and the lens midpoint 13' or 14', a line image which extends, in space, parallel with the long axis of the respective lens and with its midpoint In focus on the photosensor.
  • the diagrammatic sectional view of the head 10 shown in Figure 2 is taken in the horizontal plane which contains the photosensor 15 and the midpoints 13' and 14' of the two lenses, and shows a remote point source of light S which is also in that plane and is aligned with the photosensor 15 and the midpoint 13' of the lens 13.
  • the sensor head 10 To take a directional measurement of the source S, the sensor head 10 is rotated, and as it rotates through the illustrated position the midpoint of the line image of the source S formed by the lens 13 transits across the photosensor 15 which therefore produces an electrical output pulse. After further rotation of the head 10 through an angle ⁇ , the angle subtended at the photosensor 15 between the midpoints 13' and 14' of the two lenses, the midpoint of the line image of the source S produced by the lens 14 similarly transits across the photosensor which therefore produces a further output pulse.
  • Each output pulse is caused (by circuitry not shown) to trigger a read-out, at the Instant of Its peak value, of the Instantaneous value of the coded angular-position signal derived from the scale 12, and those read-out values are stored in a memory device (not shown).
  • the mean of these two values gives the angular position of the head 10 as the line 16, which bisects the angle ⁇ defined by the lens midpoints 13' and 14', sweeps through the source S, and this mean value, computed automatically from the two read-out values stored 1n the memory device, measures the azimuthal position of the source S relative to some predetermined zero position.
  • Figure 3(1) is a representation of the two line-image components, of the image of the source S formed by the lenses 13 and 14, which sweep across the photosensor 15 when the source S
  • the azimuthal position of the source S 1s obtained as the mean of the two read-out values stored 1n the memory; and the elevation of the source S is derivable from the difference between these two values, automatically, by computer means (not shown ) comprised by the instrument.
  • the invention enables both the azimuthal and elevatlonal components of the direction of a source object or target to be measured automatically, simply by rotating the sensor head of the instrument.
  • the source S which is the equivalent of a surveyor's staff for use with a theodolite, may conveniently be a photoluminescent diode (LED) emitting radiation in the infra-red waveband, though a source radiating in any part of the electromagnetic spectrum may be used provided, of course, that it 1s one to which the photosensor 15 is responsive.
  • the radiation output from the source S may be modulated, either to improve the signal-to-noise ratio of the signals received and processed by the measuring instrument and/or to enable each of several sources S, modulated at different frequencies, to be Individually identified, measured and memorised by the instrument.
  • the accuracy with which the transits of the image lines L and T across the photosensor can be sensed can be increased if, as shown in Figure 4, the single photosensor 15 is replaced by two photosensors 15a and 15b, one above the other, each with a photosensitive area bounded by edges which are parallel to the image lines L and T. If these photosensors have their outputs connected in opposition, then, as the image line L transits across first the photosensor 15b and then the photosensor 15a, the combined output is two opposite-going pulses, shown as (L) in Figure 5, with a zero-crossing point between them.
  • the image line T which transits first across the photosensor 15a, gives rise to the pair of pulses shown as (T) in Figure 5 which are 1n the reverse order but also have a zero-crossing point between them.
  • Using the zero-crossing points as the events which trigger read-outs from the angle encoder enables very accurate angle measurements to be obtained.
  • this configuration of photocells effectively discriminates between the leading and trailing line Images L and T, with their different "pulse signatures", and enables a false initiation of a measurement, due to the trailing beam T arriving first at the sensors, to be prevented.
  • the lenses 13 and 14 as described above are in a 1nverted-V configuration they may equally well diverge the other way, in an upr1ght-V configuration. Also, there 1s no requirement for their nearest-together ends to be closely spaced : the two lenses may be quite widely spaced apart around the circumference of the housing 11. Furthermore, as shown in Figure 6, mirrors may be employed Instead of the lenses 13 and 14. As shown 1n Figure 6, the photosensor 15 is mounted on the wall of the housing 11 at one end of a diameter 17, and faces along that diameter.
  • the mirrors 18 and 19 are skewed In opposite senses with respect to the axis Z-Z, so that the line images which they form of a distant point light source are also skewed.
  • the angle encoder from which read-outs of angular position of the detector head 10 are obtained may be of any suitable known kind.
  • it may be a moire fringe digital angle encoder which produces an electrical pulse for each unit of angular rotation, with a double-width pulse or a missing pulse to mark the zero direction of the circular scale.
  • Constant or accurately determined speed of rotation is not a requirement, and in a simple form of instrument suitable, for example, for simple surveying work, the sensor may be freely rotatable so that 1t may be spun manually to cause it to make at least one or two revolutions before co ing to rest.
  • the sensor head may be motor driven, by means of a motor incorporated 1n the Instrument, so that in use the sensor head rotates continuously at substantially constant speed.
  • a relatively coarse incremental angle encoder in combination with an electronic timer producing higher-frequency timing pulses which are used for time interpolation between the encoder pulses so as to yield the desired "fine" readings of angular position.
  • a motor-driven and continuously operating instrument 1n accordance with the invention which may be physically small and portable, may be used to determine both the position and orientation, and movement, of a body in space.
  • the body is provided for this purpose with a fixed and known array of point-source targets, and in a single sweep of the sensor head of the instrument the instantaneous direction from the instrument to each of these targets is determined.
  • the full 3-D position and orientation of the array can be measured both rapidly and automatically. If the body is in motion, each revolution of the sensor head provides updated data as to its instantaneous position.
  • a similar application of the invention exists in the spatial calibration of production robot end-effectors, obviating the need to take the robots off-line.
  • the invention may also be applied in the remote guidance of vehicles which are required to follow pre-programmed trajectories, such as tunnel-boring machines, and 1n surveying where an array of targets on a staff or rod can be used to determine the 3-D position of Its 'foot', and thus enable a ground-feature map to be produced from an unattended instrument.

Landscapes

  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Measurement Of Radiation (AREA)
EP91913367A 1990-07-20 1991-07-19 Verfahren und vorrichtung zur richtungsmessung Withdrawn EP0540594A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB909015945A GB9015945D0 (en) 1990-07-20 1990-07-20 Method and apparatus for measurement of direction
GB9015945 1990-07-20

Publications (1)

Publication Number Publication Date
EP0540594A1 true EP0540594A1 (de) 1993-05-12

Family

ID=10679378

Family Applications (1)

Application Number Title Priority Date Filing Date
EP91913367A Withdrawn EP0540594A1 (de) 1990-07-20 1991-07-19 Verfahren und vorrichtung zur richtungsmessung

Country Status (5)

Country Link
US (1) US5339088A (de)
EP (1) EP0540594A1 (de)
JP (1) JPH05508921A (de)
GB (2) GB9015945D0 (de)
WO (1) WO1992001949A1 (de)

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1473907B2 (de) * 1965-05-13 1969-10-30 Messerschmitt-BQlkow GmbH, 8000 München Vorrichtung zur Bildung eines dem Mittelwert proportionalen Zahlenwertes mit digitalen Mitteln aus zwei gegenüberliegenden Randkoordinaten eines in einer Kamera aufgefangenen Sonnenbildes
GB1410322A (en) * 1970-09-29 1975-10-15 France Armed Forces Method and apparatus for the location of a source of electro magnetic radiation
US3912397A (en) * 1973-01-08 1975-10-14 Singer Co Stellar scanning-chopping system
WO1981001195A1 (en) * 1979-10-16 1981-04-30 J Dudley Method and apparatus for determining position
US4583852A (en) * 1983-03-31 1986-04-22 The Perkin-Elmer Corporation Attitude transfer system
US4627724A (en) * 1983-07-08 1986-12-09 The United States Of America As Represented By The Secretary Of The Army Radiation scanning and detection system
JPH061197B2 (ja) * 1985-09-11 1994-01-05 株式会社東芝 スタ−スキヤナ
US4973156A (en) * 1989-10-10 1990-11-27 Andrew Dainis Linear direction sensor cameras for position measurement

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9201949A1 *

Also Published As

Publication number Publication date
GB9015945D0 (en) 1990-09-05
GB2261564B (en) 1994-08-31
WO1992001949A1 (en) 1992-02-06
US5339088A (en) 1994-08-16
JPH05508921A (ja) 1993-12-09
GB9300325D0 (en) 1993-03-10
GB2261564A (en) 1993-05-19

Similar Documents

Publication Publication Date Title
US6031606A (en) Process and device for rapid detection of the position of a target marking
EP1411371B1 (de) Vermessungs- und Positions-Vorrichtung mit aufgefächertem Lichtstrahl
CN100464159C (zh) 位置检测装置
US4717251A (en) Elevation measurement in high order surveying
US11619491B2 (en) Retroreflectors
US4234241A (en) Stereo line scanner
US10267659B2 (en) Angle detecting device and surveying instrument
WO1989000674A1 (en) An optical angle-measuring device
GB2166920A (en) Measuring angular deviation
US5761818A (en) Digital inclinometer
US4482252A (en) Calibration method and apparatus for optical scanners
US4484069A (en) Apparatus and method for sensing distance
JPS6112202B2 (de)
GB2213673A (en) Optical position finding
US5339088A (en) Method and apparatus for measurement of direction
JPH01250762A (ja) エアロゾルによる風向風速測定方法及びそのための装置
CN111580127B (zh) 具有旋转反射镜的测绘系统
CN209656068U (zh) 一种近红外星模拟器的校准装置
JPH08210854A (ja) コード化された水準測量捍の傾斜角を決定する方法
US5349183A (en) Diffraction grating rotary speed sensor having a circumferentially variable pitch diffraction grating
US6147746A (en) Process for optical measurement of relative angles
GB2256925A (en) Method and apparatus for measurement of the direction of a radiation source
SU1093892A1 (ru) Светопроекционный дальномер
CN207424266U (zh) 一种定姿定位装置
RU2147113C1 (ru) Мишень стрелкового тренажера с бегущими лучами

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19930111

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): CH DE FR GB LI NL SE

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: BRITISH TECHNOLOGY GROUP LIMITED

17Q First examination report despatched

Effective date: 19941115

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19950328